The invention provides a load cabin structure of a hypersonic aircraft and a production process, and relates to the technical field of carrier rockets, the structure comprises a load cabin shell, the load cabin shell is of a lattice structure, and the load cabin shell comprises a bottom plate and reinforcing ribs; the reinforcing ribs are located on the outer ring of the bottom plate, and a pouring cavity is formed between the reinforcing ribs and the bottom plate. The end face of the gel layer is as high as the end faces of the reinforcing ribs, so that a first circumferential surface is formed; the
fiber mixing layer wraps the first circumferential surface to form a second circumferential surface; the section of the cabin section connecting ring is in a T shape, and the cabin section connecting ring is clamped to the two ends of the bottom plate. The section of the
ceramic fiber belt is in an L shape, and the
ceramic fiber belt is installed between the bottom plate and the cabin section connecting ring. By adopting the load cabin shell of the lattice structure, the problem of light weight can be effectively solved, and the strength of the load cabin is effectively ensured through the arrangement of the reinforcing ribs and the fiber mixing layer; and meanwhile, the end part and the outer ring of the load cabin are respectively provided with a
ceramic fiber belt and a gel layer, so that the heat-proof capability of the load cabin can be effectively improved.